Effects of coflow-jet active flow control on airfoil stall

PurposeActive flow control on the NACA 0024 airfoil defined as suction-injection jet at the chord-based Reynolds number of 1.5 x 1e + 5 is studied. Design/methodology/approachThe three-dimensional incompressible unsteady Reynolds-averaged Navier-Stokes equations with the SST k-omega turbulence model are used to study the effects of coflow-jet (CFJ) on the dynamic and static stall phenomena. CFJ implementation is conducted with several momentum coefficients to investigate their turnover. Furthermore, the current work intends to analyze the CFJ performance by varying the Reynolds number and jet momentum coefficient and comparing all states to the baseline airfoil, which has not been studied in prior research investigations. FindingsIt is observed that at the momentum coefficient (C mu) of 0.06, the lift coefficients at low attack angles (up to a = 15) dramatically increase. Furthermore, the dynamic stall at the given Reynolds number and with the lowered frequency of 0.15 is explored. In the instance of C mu = 0.07, the lift coefficient curve does not show a noticeable stall feature compared to C mu = 0.05, suggesting that a more powerful stronger jet can entirely control the dynamic stall. Originality/valueFurthermore, the current work intends to analyze the CFJ performance by varying the jet momentum coefficient and comparing all states to the baseline airfoil, which has not been studied in prior research investigations.